Missile interstage ball locks, clamps, consisting of a steel strip formed segments of two parts, ball detents pirozamkov connecting and held by the tape in a rigid position on the circumference, fixing stage by means of balls on seats, components (devices) separating (compound ) rocket stages and the head portion comprising tensioning tape as a profile encompassing the circumferential flanges piroustroystvom with connecting elements, characterized in that the device is used to connect both steps in the latched position and the head of the (spacecraft), their rapid division as a team and independently, the lack of a complex multi-step operations for office, without any complex parts in the form of relaxation oscillators, coupling bolts, tape in the form of profile couplings, strain gauges, pirozamkov a hinged-clamping mechanism.
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